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DOC: correct Flight aerodynamic moment units #1149

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Merged
Gui-FernandesBR merged 1 commit into from
Aug 14, 2026
+3 −3
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DOC: correct Flight aerodynamic moment units #1149

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6 changes: 3 additions & 3 deletions rocketpy/simulation/flight.py
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Original file line number Diff line number Diff line change
Expand Up @@ -3007,19 +3007,19 @@ def R3(self):
@funcify_method("Time (s)", "M1 (Nm)", "linear", "zero")
def M1(self):
"""Aerodynamic moment acting along the x-axis of the rocket's body
frame as a function of time. Expressed in Newtons (N)."""
frame as a function of time. Expressed in Newton-metres (N·m)."""
return self.__evaluate_post_process[:, [0, 10]]

@funcify_method("Time (s)", "M2 (Nm)", "linear", "zero")
def M2(self):
"""Aerodynamic moment acting along the y-axis of the rocket's body
frame as a function of time. Expressed in Newtons (N)."""
frame as a function of time. Expressed in Newton-metres (N·m)."""
return self.__evaluate_post_process[:, [0, 11]]

@funcify_method("Time (s)", "M3 (Nm)", "linear", "zero")
def M3(self):
"""Aerodynamic moment acting along the z-axis of the rocket's body
frame as a function of time. Expressed in Newtons (N)."""
frame as a function of time. Expressed in Newton-metres (N·m)."""
return self.__evaluate_post_process[:, [0, 12]]

@funcify_method("Time (s)", "Net Thrust (N)", "linear", "zero")
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